Patent · US Active

Battery module for electrically-driven aircraft

US11148819B2 · kind B2 · utility

16Cited by
40References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 6, 2020
Grant dateOct 19, 2021
Priority date
Expiry dateOct 6, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A battery module can include multiple cell tubes, a first conductive plate, and multiple first spacers. The multiple cell tubes can accommodate multiple battery cells within the multiple cell tubes so that individual of the multiple battery cells are positioned within individual of the multiple cell tubes. The first conductive plate can include multiple first holes and electrically connect first terminals of the multiple cells. The multiple first spacers can be mounted in the multiple first holes and support the multiple tubes and the multiple cells with respect to the first conductive plate, the multiple first spacers being configured to provide thermal and electrical isolation between the multiple battery cells and the first conductive plate.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.